METHOD FOR BUTT WELDING AT LEAST TWO METAL SHEETS
20230001511 · 2023-01-05
Assignee
Inventors
Cpc classification
B23K26/242
PERFORMING OPERATIONS; TRANSPORTING
B23K37/047
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K26/242
PERFORMING OPERATIONS; TRANSPORTING
B23K37/04
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The present invention relates to a method for butt welding at least two metal sheets, namely a first metal sheet and a second metal sheet, wherein, in particular, a tailored blank is produced from the metal sheets.
Claims
1. A method for the butt-welding of a first metal sheet and a second metal sheet, wherein a tailored blank is produced from these metal sheets, wherein, in a first method step, the first metal sheet is fixed in a first clamping device and the second metal sheet is fixed in a second clamping device, wherein, in a second method step, a first edge to be welded is produced on the first metal sheet by laser cutting, wherein, in a third method step, a second edge to be welded is produced on the second metal sheet by laser cutting, wherein, in a fourth method step, the first metal sheet and the second metal sheet are positioned relative to one another for carrying out a joining process for joining, wherein, in a fifth method step, the first and second metal sheets are joined along an abutting region (11), formed by the two edges, by laser welding, wherein, in the fourth method step, the first metal sheet and the second metal sheet are positioned relative to one another, in each case while maintaining a preload brought about by the fixing produced in the first method step, either by moving the first clamping device or by moving the second clamping device or by moving the first clamping device and the second clamping device in such a way that the edge to be welded of the first metal sheet and the edge to be welded of the second metal sheet lie opposite one another so as to form a joint.
2. The method as claimed in claim 1, wherein the second, the third and the fourth method steps are carried out in such a way that, prior to the fifth method step, a groove is formed between the first edge to be welded and the second edge to be welded.
3. The method as claimed in claim 2, wherein the groove is in the form of a V groove or in the form of a Y groove or in the form of an HV groove or in the form of an HY groove.
4. The method as claimed in claim 1, wherein, during the second method step, the first edge to be welded is prepared by laser cutting in such a way that, after the laser cutting, an angle a >90° is enclosed between the first edge and a top side of the first metal sheet, said top side adjoining the first edge, wherein, during the third method step, the second edge to be welded is prepared by laser cutting in such a way that, after the laser cutting, an angle 3 > or =90° is enclosed between the second edge and a top side of the second metal sheet, said top side adjoining the second edge.
5. The method as claimed in claim 1, wherein, after the fourth method step, the first metal sheet and the second metal sheet are oriented in such a way that a first cut surface generated at the first edge lies in a first plane and a second cut surface generated at the second edge lies in a second plane, wherein the first plane and the second plane intersect when a top side of the first metal sheet and a top side of the second metal sheet lie in a third plane or in a third plane and a fourth plane, which are oriented parallel to one another.
6. The method as claimed in claim 1, wherein the second and the third method steps are carried out by laser beam cutting or by remote laser beam cutting, and wherein the fifth method step is carried out by laser beam welding or by remote laser beam welding.
7. The method as claimed in claim 6, wherein the second, the third and the fifth method steps are carried out using the same laser or using the same remote laser.
8. The method as claimed in claim 6, wherein a spacing between the remote laser and the edge or edges to be welded of the first and second metal sheets when the second, third and fifth method steps are being carried out is in each case at least 200 mm.
9. The method as claimed in claim 6, wherein the first metal sheet, in the region of its first edge to be welded, and/or the second metal sheet, in the region of its second edge to be welded, are/is treated by laser ablation by the remote laser prior to the fifth method step and in particular prior to the second and third method step, respectively.
10. The method as claimed in claim 1, wherein the metal sheets are configured in terms of their number and shape in such a way that a tailored blank closed in a ring-shaped manner is produced by the method, wherein the tailored blank closed in a ring-shaped manner is produced from at least four metal sheets.
11. The method as claimed in claim 2, wherein, in the fourth method step, the second metal sheet is positioned in relation to the first metal sheet either in such a way that, to produce a first variant of the tailored blank, a top side of the first metal sheet and a top side of the second metal sheet are brought into a first common plane and the groove is in this case formed in the direction of the top side of the second metal sheet, or in such a way that, to produce a second variant of the tailored blank, a bottom side of the first metal sheet and a bottom side of the second metal sheet are brought into a second common plane and the groove is in this case formed in the direction of the top side of the second metal sheet.
12. The method as claimed in claim 2, wherein a free volume of the groove is predetermined in such a way that said free volume is filled by a weld seam, which is generated in the fifth method step, as far as an interface, wherein the interface in the case of metal sheets whose top sides lie in a common plane is defined by this common plane, and wherein the groove is filled in such a way that a fill volume of the weld seam corresponds to the free volume of the groove, or wherein the interface in the case of metal sheets whose top sides lie at different levels is in the form of an interface which extends from the top side of the first metal sheet to the top side of the second metal sheet in a concavely curved manner, and wherein the groove is filled in such a way that a fill volume of the weld seam lies above the free volume of the groove.
13. The method as claimed in claim 12, wherein a fill volume of the weld seam in the fifth method step is increased by continuous feeding of a filler wire during the laser welding until the free volume of the groove is reached by the fill volume.
14. The method as claimed in claim 1, wherein a plurality of metal sheets are connected to form a ring, wherein, for this purpose, these metal sheets are connected by a number of weld seams which corresponds to a number of the metal sheets.
15. The method as claimed in claim 1, wherein the first edge to be welded and the second edge to be welded each have a linear profile, such that a linearly running weld seam is formed by the welding.
16. The method as claimed in claim 1, wherein the first edge to be welded and the second edge to be welded each have a two-dimensional, curved profile, such that a weld seam which runs in a two-dimensional, curved manner is formed by the welding.
17. The method as claimed in claim 1, wherein the first edge to be welded and the second edge to be welded each have a three-dimensionally curved profile, such that a weld seam which runs in a three-dimensionally curved manner is formed by the welding.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0038] Further details of the present invention will be described in the drawing by means of schematically illustrated exemplary embodiments.
[0039]
[0040]
[0041]
[0042]
[0043]
[0044]
[0045]
[0046]
[0047]
[0048]
DETAILED DESCRIPTION OF THE INVENTION
[0049]
[0050] The apparatus 1, which is shown in each of
[0051] In a first method step, the first metal sheet A is fixed in the first clamping device 3 and the second metal sheet B is fixed in the second clamping device 4 by virtue of the respective clamping jaws 3a, 3b and 4a, 4b being brought together. For this, reference is made to
[0052] As can be seen from
[0053] As can further be seen from
[0054] Provision may also be made for the third step to be carried out prior to the second step.
[0055] In the illustration of
[0056] In a fourth method step, which is effected between the states shown in
[0057] In a fifth method step, the two metal sheets A, B are then joined along the abutting region 11, formed by the two edges 9, 10, by laser welding by means of the remote laser 7. To this end, the laser beam 8 is guided along the abutting region 11 through the groove N. In the illustration of
[0058] It is important that, in the fourth method step, the first metal sheet A and the second metal sheet B are positioned relative to one another, in each case while maintaining preloads brought about by the fixing performed in the first method step by means of the clamping devices, by moving at least one of the clamping devices in such a way that the edge to be welded 9 of the first metal sheet A and the edge to be welded 10 of the second metal sheet B lie opposite one another so as to form a joint 13, which forms the groove N.
[0059] The second, the third and the fourth method step are carried out in such a way that, prior to the fifth method step, the groove N is formed between the first edge to be welded 9 and the second edge to be welded 10. To this end, both the first metal sheet A and the second metal sheet B are cut by means of the laser beam 8 in such a way that both the first edge 9 and the second edge 10 are produced in the form of an oblique edge.
[0060]
[0061] Both in the first method variant and in the second method variant, the one remote laser 7 is used to carry out both the two laser cuts and the welding.
[0062] As an alternative, provision is also made for the clamping devices to be in the form of magnetically operating clamping apparatuses or in the form of pneumatically operating clamping apparatuses.
[0063]
[0064] It holds true for all four groove variants N1 to N4 shown in
[0066] A2 or A3 or A4, respectively, the top side adjoining the first edge 9.1 or 9.2 or 9.3 or 9.4, respectively, [0067] in that, during the third method step, the second edge to be welded 10.1 or 10.2 or 10.3 or 10.4, respectively, is prepared by means of laser cutting in such a way that, after the laser cutting, an angle 31 or 32 or 34 or 34, respectively, > or =90° is enclosed between the second edge 10.1 or 10.2 or 10.3 or 10.4, respectively, and a top side 16.1 or 16.2 or 16.3 or 16.4, respectively, of the second metal sheet B1 or B2 or B3 or B4, respectively, the top side adjoining the second edge 10.1 or 10.2 or 10.3 or 10.4, respectively.
[0068] Correspondingly, it holds true that, after the fourth method step, the first metal sheet A1, A2, A3, A4 and the second metal sheet B1, B2, B3, B4 are oriented in such a way that a first cut surface 17.1, 17.2, 17.3, 17.4 generated at the first edge 9.1, 9.2, 9.3, 9.4 lies in a first plane E1, E2, E3, E4 and a second cut surface 18.1, 18.2, 18.3, 18.4 generated at the second edge 10.1, 10.2, 10.3, 10.4 lies in a second plane F1, F2, F3, F4, wherein the first plane and the second plane E1, F1, respectively, or E2, F2, respectively, or E3, F3, respectively, or E4, F4, respectively, intersect and thus are not parallel to one another when a top side 15.1, 15.2, 15.3, 15.4 of the first metal sheet A1, A2, A3, A4 and a top side 16.1, 16.2, 16.3, 16.4 of the second metal sheet B1, B2, B3, B4 both lie in a third plane G1, G2, G3 or, as illustrated in
[0069]
[0070] In the variants shown in
[0071] In the variant shown in
[0072] As mentioned in relation to
[0073] A spacing d7 (see
[0074] In all of the described method variants, provision is optionally also made for the first metal sheet A, in the region of its first edge to be welded 9, and/or the second metal sheet B, in the region of its second edge to be welded 10, to be treated, and thus, in particular, to be cleaned, by laser ablation by means of the remote laser 7 prior to the fifth method step and, in particular, prior to the second and third method step, respectively.
[0075] In the case of the metal sheets A, B shown
[0076] In the case of the metal sheets A5, B5 shown
[0077] In the case of the metal sheets A6, B6 shown in
[0078] According to an embodiment variant of the method that is not illustrated, provision is also made for the metal sheets to be configured in terms of their number and shape in such a way that a tailored blank closed in a ring-shaped manner is produced by the method, wherein the tailored blank closed in a ring-shaped manner is produced, in particular, from at least six metal sheets. The apparatus on which this method is carried out then comprises a corresponding number of clamping devices and, where appropriate, a number of laser devices which corresponds to the number of metal sheets. As an alternative, a laser device may also be provided which performs the laser cutting and laser welding of all the metal sheets and which is displaced correspondingly for this purpose, provision also being able to be made that, as an alternative or in addition, the clamping devices are displaced in order to bring the laser device and the metal sheets into position relative to one another. In such a method, to produce a component or tailored blank, a plurality of weld seams are then generated on the component or tailored blank by the same laser device. Such a method reduces the construction outlay for an apparatus for producing such components or tailored blanks considerably.
[0079] In
[0080] To this end, it is provided in the method described in relation to
[0083] In order to position the metal sheets A7, B7 and A8, B8, respectively, relative to one another, at least one of the clamping devices (not illustrated) in which the metal sheets are clamped during all of the laser processing steps is additionally displaced in the above-mentioned third spatial direction z or z′.
[0084] In this case, laser cutting of the first metal sheet A7 and of the second metal sheet B7 so as to form edges 9.7 and 10.7 is effected in such a way that a Y seam is formed as weld seam 12.7 between the metal sheets A7, A8 after the laser welding.
[0085] In this case, laser cutting of the first metal sheet A8 and of the second metal sheet B8 so as to form edges 9.8 and 10.8 is effected in such a way that a V seam is formed in each case as weld seam 12.8 between the metal sheets A8, B8 after the laser welding.
[0086] In principle, it is provided for all embodiment variants of tailored blanks that—as, for example, shown in
[0087] If provision is made of laser welding with filler wire, this is taken into account in the predetermination of the free volume of the groove, and the free volume of the groove is correspondingly dimensioned to be greater. Correspondingly, a fill volume of the weld seam in the fifth method step is increased by continuous feeding of a filler wire during the laser welding until the free volume of the groove is reached by the fill volume.
[0088] In principle, provision is made in all of the described method variants for the first clamping device 3 and/or the second clamping device 4 to be oriented relative to one another on the basis of coordinates detected in relation to a first laser cut on the first metal sheet A, A1 to A8 and in relation to a second laser cut on the second metal sheet B, B1 to B8.
[0089]
[0090] The apparatus 101 shown in schematic plan view in
[0091] In the illustration of
[0092] One and the same remote laser 107 is used to carry out both the laser cutting and the laser welding on all of the metal sheets A9, B9, C9 and D9. It goes without saying that this method can also be used to connect more than four metal sheets to form a ring. The apparatus is then equipped with a sufficient number of clamping devices. In the case of larger metal sheets, provision may also be made for the metal sheets to be clamped by means of at least two clamping devices, as is shown in
[0093] Furthermore, provision is in principle also made in the described embodiments, as an alternative, for a conventional laser to be used instead of the remote laser.
List of Reference Designations
[0094] 1 Apparatus [0095] 2 Base [0096] 3 First clamping device [0097] 3a, 3b Clamping jaw of 3 [0098] 4 Second clamping device [0099] 4a, 4b Clamping device of 4 [0100] 5 Laser device [0101] 6 Head of 5 [0102] 7 Remote laser in 6 [0103] 8 Laser beam [0104] 9, 9.1-9.8 Edge to be welded of A [0105] 10, 10.1-10.8 Edge to be welded of B [0106] 11 Abutting region [0107] 12, 12.1-12.5, 12.7,12.8 Weld seam [0108] 13, 13.1-13.4 Joint [0109] 14 Filler wire [0110] 15, 15.1-15.7 Top side of A [0111] 16, 16.1-16.8 Top side of B [0112] 17.1-17.4 Cut surface on A1-A4 [0113] 18.1-18.4 Cut surface on B1-B4 [0114] 19.8 Bottom side of A8 [0115] 20.8 Bottom side of B8 [0116] 101 Further apparatus [0117] 102 Base [0118] 103-1 to 103-5 Clamping device [0119] 105 Laser device [0120] 106 Head of 5 [0121] 107 Remote laser in 6 [0122] 108 Laser beam [0123] A, A1-A9 First metal sheet [0124] B, B1-B9 Second metal sheet [0125] C9 Third metal sheet [0126] D9 Fourth metal sheet [0127] E1-E4 First plane [0128] F1-F4 Second plane [0129] G1-G4 Third plane [0130] H4 Fourth plane [0131] I7 Common plane of 15.7 and 16.7 [0132] I8 Common plane of 15.8 and 16.8 [0133] N, N1-N8 Groove [0134] R9 Ring [0135] T, T1-T9 Tailored blank [0136] A9-1; A9-2 Edge of A9 [0137] B9-1; B9-2 Edge of B9 [0138] C9-1, C9-2 Edge of C9 [0139] D9-1, D9-2 Edge of D9 [0140] AB9, BC9, CD9, DA9 Weld seam [0141] FV1-FV4; FV7, FV8 Free volume of N1-N4, N7, N8 [0142] FV12.1-FV12.4 Fill volume of 12.1-12.4 [0143] FV12.7, FV12.8 Fill volume of 12.7, 12.8 [0144] GF1-GF4, GF7, GF8 Interface [0145] d7 Spacing between 7 and 9 or 10 [0146] x, x′, y, y′, z, z′ Spatial direction [0147] α1-α4 Angle between 9.1-9.4 and [0148] 15.1-15.4 [0149] β1- β4 Angle between 10.1-10.4 and [0150] 16.1-16.4